A technique based on superposition of tricyclic solutions has been proposed for smoothing free-flight angular motion. When incorporated into a conventional tricyclic data reduction program, the method is convenient to use and does not require a separate smooting routine. Tricyclic motion components determined in the smoothing process can be related to effects of individual nonlinearities on the motion.
Reference:
Beyers, ME. 1975. Technique for smoothing free-flight oscillation data. Journal of Spacecraft and Rockets, vol 12(5), pp 318-319
Beyers, M. (1975). Technique for smoothing free-flight oscillation data. http://hdl.handle.net/10204/2230
Beyers, ME "Technique for smoothing free-flight oscillation data." (1975) http://hdl.handle.net/10204/2230
Beyers M. Technique for smoothing free-flight oscillation data. 1975; http://hdl.handle.net/10204/2230.
